| 摘要 |
<p>A convertiplane (1) having a fuselage (2) with a first axis (3); and two rotors (14) having respective shafts (42) and fitted to a wing (4) having a fixed portion (5) connected to the fuselage (2), and a movable portion (6) which supports the rotors (14), is connected to the fixed portion (5) to rotate about a second axis (7) crosswise to the first axis (3) and to the shafts (42) of the rotors (14), and is formed in one piece defined by two half-wings (8) located on opposite sides of the fixed portion (5) and each supporting a respective rotor (14), and by an elongated member (9) extending along the whole wing (4) and connecting the two half-wings (8); the rotors (14) being powered by a motor (13) via a transmission (12) comprising a transmission shaft (41) connecting the shafts (42) of the rotors (14) and coaxial with the second axis (7).</p> |
